On this page
Text · 58
From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document. © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0486, the docket of AD 2019-18-06. Not covered by OpenAirDocs’ CC0 dedication.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '9f7afaa97c94b547c905828aaee48c077518154b059ff54f0a6b08d4fd73e65c' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '9f7afaa97c94b547c905828aaee48c077518154b059ff54f0a6b08d4fd73e65c' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 1
CONF ALL AIRBUS S.A.S.
Customer Services T echnical Data Support and Services 31703 Blagnac Cedex FRANCE
The content of this document is the property of Airbus.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus.
MANDATORY MANDATORY MANDATORY ATA SYSTEM: 25 TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS-
INTRODUCE NEW FIXATION FOR POHSC MODIFICATION No.:
160418K30484
A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 2 ATA SYSTEM: 25 TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS-
INTRODUCE NEW FIXATION FOR POHSC
REVISION TRANSMITTAL SHEET This page transmits Revision No. 01 of Service Bulletin No. A320-25-1BGJ.
A. ADDITIONAL WORK Additional Work is required by this revision for aircraft modified by the original issue of this Service Bulletin.
Unless otherwise stated by an Airworthiness Directive, AIRBUS recommends the Additional Work to be accomplished within one year after the issue of this revision.
The Additional Work describes:
- Check of dimensions of the Threaded Pins against tolerances
- Replacement of the Threaded Pins and Nuts if necessary.
B. REASON Revision No. 01 issued to:
- Transform Service Bulletin data from ATA iSpec 2200 norm to ASD S1000D norm
- Update the dimensions of the Threaded Pins
- Add an Additional Work T ask for aircraft modified by the original issue of this Service Bulletin.
C. CHANGES
SERVICE BULLETIN General Revised text and layout changes of this revision are not identified with revision bars.
D. FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
E. HISTORY OF PREVIOUS REVISIONS No previous revision F. REVISION SEQUENCE ORIGINAL: Dec 19/17 REVISION No. : 01 - Aug 21/18
A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 3 ATA SYSTEM: 25 TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS-
INTRODUCE NEW FIXATION FOR POHSC
SUMMARY This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR 160418K30484 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
NOTE: This modification related to an Airworthiness issue has been classified by Airbus and confirmed by EASA as minor in accordance with EU Part 21.A.91. As such, this minor change is handled by Airbus under its Design Organisation Approval No.
EASA.21J.031.
B. REASON
(1) History Several operators have reported loose or missing screws at the X-brackets, Y- brackets and connecting plates of their Over Head Stowage Compartments (OHSC).
Investigations and a sampling program have shown that fuselage deflections (due to pressure and temperature differences caused during a regular flight cycle) lead to loads on the secondary X-load path in the OHSC. This is the root cause of the screws loosening. The aircraft affected by this Service Bulletin are equipped with the Pivoting Over Head Stowage Compartment (POHSC) design.
(2) Objective/Action This Service Bulletin replaces the current screws in the X-brackets, Y-brackets and connecting plates with threaded pins with applied micro-encapsulated coating and additional self-locking nuts.
(3) Advantages The embodiment of this Service Bulletin will improve the robustness of the POHSC fixation system thus avoiding further unscheduled maintenance in this area.
(4) Operational/Maintenance Consequences None C. GENERAL EVALUATION
EVALUATION TABLE COMPLIANCE MANDATORY COST SAVING No
A/C OPERATION
AFFECTED
NO VENDOR SB NO
CANCELS INSPECTION SB NO ETOPS AFFECTED NO
PAX COMFORT AFFECTED NO POTENTIAL AD YES
A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 4
EVALUATION TABLE
RELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NO
LIFE LIMIT NO LINE MAINTENANCE AFFECTED NO NOTE: Service Bulletin must be accomplished.
D. MAINTENANCE CONFIGURATION No specific aircraft maintenance configuration required.
E. MATERIAL PRICE INFORMATION
(1) Modification
(a) T ask set A320-A-25-XX-1BGJ-01000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS Part kit 251BGJD01R01 1 3950.00 USD Threaded pins, washers, nuts
(2) Inspection - Additional Work for Aircraft Modified by Revision No. 00
(a) T ask set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS Components See SB See Note Threaded pin, nut, washer NOTE: Price information to be acquired by the given supplier.
F. APPLICABILITY This Service Bulletin is applicable to this (these) operator(s):
DAL LAN WOW G. CONCURRENT REQUIREMENTS None H. NATURE OF THE WORK
(1) Modification
(a) T ask set A320-A-25-XX-1BGJ-01000-93AA-A Modification
AIRCRAFT YES
EQUIPMENT NO
(2) Inspection - Additional Work for Aircraft Modified by Revision No. 00
(a) T ask set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00
AIRCRAFT YES
EQUIPMENT NO
A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 5 I. MANPOWER
(1) Modification
(a) T ask set A320-A-25-XX-1BGJ-01000-93AA-A Modification
MANPOWER TOTAL MAN-HOURS 42.00 h ELAPSED TIME (HOURS) 14.50 h
(2) Inspection - Additional Work for Aircraft Modified by Revision No. 00
(a) T ask set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00
MANPOWER TOTAL MAN-HOURS 18.50 h ELAPSED TIME (HOURS) 9.25 h
A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY Figure ICN-A320-A-25XX1BGJ-A-FAPE3-000BI-A-001-01 SHEET 1/1 REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 General Overview Page 6 J. GENERAL OVERVIEW
CONF ALL A Z230 Z250 Z260 Z240 FR21 FR66 A TYPICAL A320
FAMILY AIRCRAFT NOTE:
AREA OF MODIFICATION ICN-A320-A-25XX1BGJ-A-FAPE3-000BI-A-001-01
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 7 ATA SYSTEM: 25 TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS-
INTRODUCE NEW FIXATION FOR POHSC
1. PLANNING INFORMATION A. APPLICABILITY NOTE: This Service Bulletin is only applicable to aircraft on which MOD No. 156853K17985 is embodied.
(1) Models ON A/C 6923, 7031, 7061, 7112, 7149, 7165, 7214, 7233, 7237, 7239, 7268, 7281, 7287, 7293, 7298, 7304, 7327, 7364, 7373, 7379, 7381, 7433, 7436, 7441, 7479, 7546, 7592, 7672, 7707, 7709, 7765, 7777, 7840, 7845, 7885, 7896, 7943, 7973, 8026, 8036, 8040, 8063, 8078, 8080, 8134 321-211
CONF ALL
(2) Applicability by MSN 6923 7031 7061 7112 7149 7165 7214 7233 7237 7239 7268 7281 7287 7293 7298 7304 7327 7364 7373 7379 7381 7433 7436 7441 7479 7546 7592 7672 7707 7709 7765 7777 7840 7845 7885 7896 7943 7973 8026 8036 8040 8063 8078 8080 8134
(3) MSN by configuration
MSN CONFIGURATION 6923 7031 7061 7112 7149 7165 7214 7233 7237 7239 7268 7281 7287 7293 7298 7304 7327 7364 7373 7379 7381 7433 7436 7441 7479 7546 7592 7672 7707 7709 7765 7777 7840 7845 7885 7896 7943 7973 8026 8036 8040 8063 8078 8080 8134 001
(4) Configuration definition Configuration 001 CONF 001 is applicable for all the aircraft affected by this Service Bulletin as a standard configuration.
B. CONCURRENT REQUIREMENTS None C. REASON
(1) History Several operators have reported loose or missing screws at the X-brackets, Y- brackets and connecting plates of their Over Head Stowage Compartments (OHSC).
Investigations and a sampling program have shown that fuselage deflections (due to pressure and temperature differences caused during a regular flight cycle) lead to loads on the secondary X-load path in the OHSC. This is the root cause of the screws loosening. The aircraft affected by this Service Bulletin are equipped with the Pivoting Over Head Stowage Compartment (POHSC) design.
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 8
(2) Objective/Action This Service Bulletin replaces the current screws in the X-brackets, Y-brackets and connecting plates with threaded pins with applied micro-encapsulated coating and additional self-locking nuts.
(3) Advantages The embodiment of this Service Bulletin will improve the robustness of the POHSC fixation system thus avoiding further unscheduled maintenance in this area.
(4) Operational/Maintenance Consequences None D. DESCRIPTION T o accomplish this Service Bulletin it is necessary to:
(1) Modification
(a) T ask set A320-A-25-XX-1BGJ-01000-93AA-A Modification 1 Modify the Left Hand (LH) Pivoting Over Head Stowage Compartments (POHSC's) 2 Modify the Right Hand (RH) Pivoting Over Head Stowage Compartments (POHSC's)
(2) Inspection - Additional Work for Aircraft Modified by Revision No. 00
(a) T ask set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00 1 Check Dimension of the Threaded Pins of the Left Hand (LH) Pivoting Over Head Stowage Compartments (POHSC's) 2 Check Dimension of the Threaded Pins of the Right Hand (RH) POHSC's E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale Accomplishment of this Service Bulletin must be done within 72 months after issuance of the original issue of this Service Bulletin.
This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds given but reference should be made to the AD for confirmation of the mandated accomplishment timescale.
F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031.
If an aircraft listed in the applicability has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.
G. MANPOWER
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 9 The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included.
(1) Modification
(a) T ask set A320-A-25-XX-1BGJ-01000-93AA-A Modification
PREPARATION Job Set-up 8.00 h
PROCEDURE Modify the Left Hand (LH) Pivoting Over Head Stowage Compartments (POHSC's)
13.00 h Modify the Right Hand (RH) Pivoting Over Head Stowage Compartments (POHSC's)
13.00 h
PREPARATION FOR TEST None TEST None
CLOSE-UP Close-Up 8.00 h TOTAL MAN-HOURS 42.00 h ELAPSED TIME (HOURS) 14.50 h NOTE: For an explanation of the man-hours and elapsed time, refer to the Gantt Chart given in Appendix Manpower Gantt Chart.
(2) Inspection - Additional Work for Aircraft Modified by Revision No. 00
(a) T ask set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00
PREPARATION Job Set-up 8.00 h
PROCEDURE Check Dimension of the Threaded Pins of the Left Hand (LH) Pivoting Over Head Stowage Compartments (POHSC's)
1.25 h Check Dimension of the Threaded Pins of the Right Hand (RH) POHSC's
1.25 h
PREPARATION FOR TEST None TEST None
CLOSE-UP Close-up 8.00 h TOTAL MAN-HOURS 18.50 h ELAPSED TIME (HOURS) 9.25 h
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 10 NOTE: The minimum man-hours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional man-hours can apply.
NOTE: For an explanation of the man-hours and elapsed time, refer to the Gantt Chart given in Appendix Manpower Gantt Chart - Additional Work H. WEIGHT AND BALANCE The weight and balance estimates given in this Service Bulletin are based on the Manufacturer's Empty Weight (MEW) and do not include operator's items. For the definition of MEW and operator's items, refer to Ref. WBM.
Manufacturer's Empty Weight +0.1 kg (+0.220 lb) Effect on Balance +1.6 kg.m (+11.573 lb.ft) I. ELECTRICAL LOAD DATA Not changed J. REFERENCES
(1) Modification
(a) T ask set A320-A-25-XX-1BGJ-01000-93AA-A Modification
AIRCRAFT MAINTENANCE MANUAL (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 T ask 12-34-24-869-002 T ask 25-23-48-000-001 T ask 25-23-48-400-001 T ask 25-24-41-000-001 T ask 25-24-41-400-001 T ask 25-25-11-000-001 T ask 25-25-11-400-001
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM) 20-55-00
WEIGHT AND BALANCE MANUAL (WBM)
STANDARDS MANUAL (SM)
(2) Inspection - Additional Work for Aircraft Modified by Revision No. 00
(a) T ask set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00
AIRCRAFT MAINTENANCE MANUAL (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 T ask 12-34-24-869-002 T ask 25-23-48-000-001 T ask 25-23-48-400-001 T ask 25-24-41-000-001 T ask 25-24-41-400-001 T ask 25-25-11-000-001 T ask 25-25-11-400-001
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM) 20-55-00
WEIGHT AND BALANCE MANUAL (WBM)
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 11
STANDARDS MANUAL (SM) K. PUBLICATION AFFECTED
AIRCRAFT MAINTENANCE MANUAL (AMM)
ILLUSTRATED PART CATALOG (IPC) L. INDUSTRY SUPPORT INFORMATION AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at no charge for orders placed before Oct 31/23.
AIRBUS will not credit the man-hours indicated in this Service Bulletin. They remain at operator's charge.
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department: monitored.retrofit@airbus.com.
A318/A319/A320/A321
SERVICE BULLETIN REV 00 Dec 19/17 A320-25-1BGJ REV 01 Aug 21/18 Page 12
2. MATERIAL INFORMATION A. MATERIAL APPLICABILITY Material for task set A320-A-25-XX-1BGJ-01000-93AA-A Modification
MATERIAL QTY SEE NOTES Part kit 251BGJD01R01 1 Material for task set A320-A-25-XX-1BGJ-01000-93BA-A Inspection - Addtional Work for Aircraft Modified by Revision No. 00
MATERIAL QTY SEE NOTES Components See SB (1) (2)
NOTE(S)
(1): One COMPQ01 must be ordered for each replacement Threaded Pin, Item 10, Nut, Item 12 and Washer, Item 15.
(2): One COMPQ02 must be ordered for each replacement Threaded Pin, Item 13, Nut, Item 14 and Washer, Item 11.
B. TOOLING No tools C. CONSUMABLES No consumables D. LIST OF NEW PARTS Part kit 251BGJD01R01 Cost 3950.00 USD Availability 180 d (calendar days from receipt of order)
NOTE(S) The availability given above is the standard lead-time from the date of your purchase order. If items are required before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions. The latest valid price and lead-time for ordering purposes shall be obtained through the AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
Procurement address D4296 AIRBUS Material, Logistics and Suppliers
ATP II B Hein-Sass-Weg 24 21129 HAMBURG
GERMANY Phone: +49 40 743 51660 E-mail: airbus.kit@airbus.com Internet: http://spares.airbus.com
NOTE(S) Customers with aircraft shown in the applicability of this Service Bulletin should send a purchase order to AIRBUS at the address given above and quote the number of this Service Bulletin.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES 10 FAS000033-100 198 PIN 11 NAS1149CN832R 670 WASHER